Method for process for producing fully ceramic microencapsulated fuels containing tristructural-isotropic particles with a coating layer having higher shrinkage than matrix
US-2021304908-A1 · Sep 30, 2021 · US
US12428350B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-12428350-B2 |
| Application number | US-202117185909-A |
| Country | US |
| Kind code | B2 |
| Filing date | Feb 25, 2021 |
| Priority date | Feb 19, 2018 |
| Publication date | Sep 30, 2025 |
| Grant date | Sep 30, 2025 |
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Methods of forming composite materials, composite materials, and articles. The composite materials may include electromagnetic shielding materials. The methods may include providing a mixture of ultra-high temperature ceramic particles and a liquid preceramic precursor, curing the mixture to form a solid mixture, forming particles of the solid mixture, and pressing the particles into a mold.
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The invention claimed is: 1. A composite material comprising: a plurality of particles of a solid mixture, the solid mixture comprising ultra-high temperature ceramic particles and a polymer-derived ceramic; wherein the ultra-high temperature ceramic particles are at least partially coated with the polymer-derived ceramic; and wherein the plurality of particles is a plurality of discrete particles. 2. The composite material of claim 1 , wherein each discrete particle of the plurality of particles of the solid mixture comprises— (a) a core region comprising an amount of the ultra-high temperature ceramic particles, and (b) a surface region comprising an amount of polymer-derived ceramic; wherein for each of the particles of the solid mixture— (i) the amount of the ultra-high temperature ceramic particles of the core region includes at least 75%, by weight, of the ultra-high temperature ceramic particles that are present in each particle of the solid mixture, and (ii) the amount of the polymer-derived ceramic of the surface region includes at least 75%, by weight, of the polymer-derived ceramic that is present in each particle of the solid mixture. 3. The composite material of claim 1 , wherein the ultra-high temperature ceramic particles have a melting temperature of at least 2,000° C. 4. The composite material of claim 1 , wherein the ultra-high temperature ceramic particles have at least one of the following properties: [1] an elastic modulus of at least 500 GPa, [2] a hardness of at least 20 GPa, [3] an electrical conductivity of at least 10 7 S/m, or [4] a thermal conductivity of about 60 to about 120 W/m*K. 5. The composite material of claim 1 , wherein the ultra-high temperature ceramic particles are selected from the group consisting of a boride, a carbide, and a nitride. 6. The composite material of claim 1 , wherein the ultra-high temperature ceramic particles comprise HfB 2 , ZrB 2 , TiB 2 , NbB 2 , TaB 2 , or a combination thereof. 7. The composite material of claim 1 , wherein the ultra-high temperature ceramic particles comprise TaC, HfC, ZrC, NbC, TiC, or a combination thereof. 8. The composite material of claim 1 , wherein the ultra-high temperature ceramic particles comprise TaN, HAN, TIN, ZrN, NbN, or a combination thereof. 9. An article comprising: one or more surfaces, and the composite material of claim 1 ; wherein the composite material is arranged on the one or more surfaces of the article. 10. The article of claim 9 , wherein the composite material is an electromagnetic shielding material. 11. The article of claim 9 , wherein the article is at least part an aircraft or a submarine. 12. The article of claim 11 , wherein the at least part of the aircraft comprises a nosecone.
based on non-oxide ceramics · CPC title
Fibres, filaments, whiskers, platelets, or the like · CPC title
Milling · CPC title
Mechanical properties, e.g. fracture toughness, hardness, Young's modulus or strength · CPC title
Making the green bodies or pre-forms by moulding · CPC title
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